Unmanned helicopter airborne pod convenient to install
By designing an unmanned helicopter onboard pod with a retractable connecting shaft and a clamp, the problem of poor adaptability to unmanned helicopters of different specifications was solved, achieving low-cost and highly adaptable simulation training results.
Patent Information
- Application Number
- CN202520151216.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-22
- Publication Date
- 2025-12-26
- Estimated Expiration
- 2035-01-22
AI Technical Summary
Existing unmanned helicopter onboard pods cannot adapt to unmanned helicopters of different sizes and shapes, resulting in poor adaptability and high manufacturing costs.
An easy-to-install unmanned helicopter airborne pod was designed, which is connected to the unmanned helicopter support using a telescopic connecting shaft and a clamp. Stability is improved by the triangular distribution of installation support points, and the angle of the simulated missile clamp can be adjusted to adapt to unmanned helicopters of different specifications.
It achieves high adaptability of airborne pods, reduces manufacturing costs, and is easy to install and disassemble, making it suitable for simulation training of unmanned helicopters of different specifications.
Smart Images
Figure CN223721146U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model mainly relates to unmanned helicopter pod, concretely relates to a kind of unmanned helicopter airborne pod of easy installation. BACKGROUND
[0002] With the rapid development of unmanned aerial vehicle and the change of modern military operation mode, unmanned helicopter is widely used in military field, mainly including reconnaissance and surveillance, attack and combat, electronic warfare, battlefield management and battlefield material transportation etc. Attack unmanned helicopter can carry missile, rocket, bomb and other weapons, carry out accurate attack, effectively reduce personnel casualty and combat cost, greatly improve combat effectiveness.
[0003] To improve training efficiency and intuitively experience unmanned helicopter attack feeling, airborne pod can be installed on unmanned helicopter after completion, to facilitate the installation of different simulated rocket, and specific rocket launch data can be obtained through actual experiment.
[0004] The inventor found the following defects in the specific embodiment operation process:
[0005] As the current unmanned helicopter size specification is different, it needs to adapt different airborne pod, and the adaptability of traditional airborne pod is limited, different rocket simulation pod needs to be developed for different models, and it cannot be adaptively installed according to the size or shape of unmanned helicopter, resulting in poor adaptability of current unmanned helicopter airborne pod and high production cost.
[0006] It should be noted that the above content belongs to the technical cognition of the inventor, and due to the complexity and complexity of the technical content in the field, the above content of the present application does not necessarily constitute the prior art. CONTENT OF THE UTILITY MODEL
[0007] 1. Technical problem to be solved by the utility model:
[0008] The utility model provides a kind of unmanned helicopter airborne pod of easy installation to solve the technical problems existing in the above background technology.
[0009] 2. Technical scheme:
[0010] In order to achieve the above object, the utility model provides technical scheme for: a unmanned helicopter airborne pod convenient to install, including first fixed plate, one side of first fixed plate top connects L shape fixed plate, L shape fixed plate bottom rotatory connection simulation missile clamping portion, the outside of L shape fixed plate top is detachable connection rotatory connector, rotatory connector top detachable connection telescopic connecting shaft one end, telescopic connecting shaft other end detachable connection combined with hoop, first fixed plate outside symmetry connection rotatory connector, telescopic connecting shaft and combined with hoop, combined with hoop and unmanned helicopter support detachable connection, when the device is installed, select the appropriate unmanned helicopter support as the support installation point, unmanned helicopter support can select the part of high structural strength landing gear, original carrier platform, body frame etc convenient to install, after selecting the installation support point which is relatively triangular distribution on unmanned helicopter support, measure the distance size of three installation support points to the corresponding installation hole of the pod, then adjust the telescopic connecting shaft to the corresponding length, the size error can be controlled within 3cm, connect the connecting end of combined with hoop with telescopic connecting shaft, finally connect the clamping end of combined with hoop with unmanned helicopter support, after fine adjustment, make L shape fixed plate and unmanned helicopter horizontal plane horizontal, because three telescopic connecting shafts are triangularly arranged, the stability of L shape fixed plate can be improved, so the stability of simulation missile clamping portion can be ensured, which is convenient for subsequent simulation missile experiment, and the length of telescopic connecting shaft can be adjusted according to the condition of unmanned helicopter support, and then be suitable for unmanned helicopters of different specifications, the manufacturing cost is low, and the installation and dismounting are convenient, and be suitable for simulation bomb release training of unmanned helicopters of different specifications.
[0011] Further, the rotatory connector includes a fixed pin, one end of the fixed pin is threadedly connected with a first bolt, the other end of the fixed pin is connected with a concave clamping piece, and the concave clamping piece is detachably connected with the telescopic connecting shaft.
[0012] Further, the telescopic connecting shaft is threadedly connected with a first connecting piece at both ends, the other end of the first connecting piece is integrally formed with a rotating block, and the rotating block is detachably connected with the concave clamping piece through a bolt.
[0013] Further, the telescopic connecting shaft includes a first telescopic pipe, one end of the first telescopic pipe is slidably inserted into a second telescopic pipe, fixed holes are spaced apart on the first telescopic pipe and the second telescopic pipe, and the fixed holes are connected through screws.
[0014] Further, the combined hoop includes symmetrically arranged arc-shaped clamping pieces, clamping holes are arranged on both sides of the arc-shaped clamping pieces, and one of the clamping holes is connected with the rotating block through a bolt.
[0015] Further, a buffer material is arranged at the connection between the arc-shaped clamping piece and the unmanned helicopter support.
[0016] Further, the simulation missile clamping part comprises a mounting block, two ends of the mounting block are connected with the L-shaped fixing plate and the first fixing plate through rotating columns, assembly holes are spaced apart on the mounting block, a side of the assembly holes is connected with a missile mounting pipe, and the missile mounting pipe is placed with simulation rockets.
[0017] Further, the missile mounting pipe is provided with a fixing notch, and the fixing notch is threadedly connected with a limiting bolt.
[0018] Further, the L-shaped fixing plate is provided with an arc-shaped groove on a side, the arc-shaped groove is matched with a locking screw, and the locking screw is connected with the mounting block.
[0019] 3. Beneficial effects:
[0020] Compared with the prior art, the technical scheme has the beneficial effects that:
[0021] The utility model discloses reasonable in design, and utilize the telescopic connecting shaft of different length that can be stretched cooperation combination hoop, can be connected with the unmanned helicopter support of different size, improve the adaptive performance of airborne pod, and further reduce the manufacturing cost of airborne pod.
[0022] Through setting up the simulation missile clamping part that can rotate and the locking screw that can be locked, the missile mounting pipe can be set up at different angles with the ground, and further adapt to different scale simulation training and different scale flight height, and the adaptive performance of the device is further improved.
[0023] It should be noted that the structures not introduced in the utility model are the same as the prior art or can be realized by using the prior art, and do not involve the design points and improvement direction of the utility model, and details are not repeated here. DRAWINGS
[0024] Figure 1 It is the structural schematic diagram of the utility model;
[0025] Figure 2 It is the structural schematic diagram of the telescopic connecting shaft of the utility model;
[0026] Figure 3 It is the structural schematic diagram when the utility model is connected with the rotating connecting piece.
[0027] Figure 4 It is the structural schematic diagram when the utility model is connected with the combination hoop.
[0028] REFERENCE NUMERALS:
[0029] 1, the first fixed plate; 2, L-shaped fixed plate; 21, arc-shaped groove; 22, locking screw; 3, simulated missile clamping part; 31, mounting block; 32, rotating column; 33, assembly hole; 34, ammunition mounting pipe; 341, limiting bolt; 4, rotating connecting piece; 41, fixed pin; 42, first bolt; 43, concave clamping piece; 5, telescopic connecting shaft; 51, first connecting piece; 52, rotating block; 53, first telescopic pipe; 54, second telescopic pipe; 55, fixed hole; 6, combined hoop; 61, arc-shaped clamping piece; 62, clamping hole. DETAILED DESCRIPTION
[0030] In order to facilitate the understanding of the present application, the present application will be described more fully below with reference to the accompanying drawings, in which several embodiments of the present application are given. However, the present application can be realized in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the present application more thorough and comprehensive.
[0031] In the description of the present application, it should be understood that the orientations or positional relationships indicated by the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "page", "bottom", "inner", "outer", "clockwise", "counterclockwise" are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, and therefore cannot be understood as indicating or implying that the devices or elements indicated must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as limiting the present application.
[0032] In addition, the terms "first" and "second" are only for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" can explicitly or implicitly include one or more of the features. In the description of the present application, the meaning of "multiple" is two or more, unless otherwise specifically limited.
[0033] In the present application, unless otherwise specifically defined and limited, the terms "mounting", "connection", "connection", "fixing", "provided with", "provided in" and the like should be understood in a broad sense, for example, it can be fixedly connected, or it can be detachably connected, or it can be integrally connected; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium; it can be the communication between two elements inside. For those skilled in the art, the specific meaning of the above terms in the present application can be understood according to the specific circumstances.
[0034] It should be noted that the structures not introduced in the present application do not involve the design points and improvement direction of the present application, and can adopt the existing technology known by those skilled in the art. Embodiments
[0035] Referring to the drawings Figures 1-4 A unmanned helicopter airborne pod convenient to install, including first fixed plate 1, one side of the top of the first fixed plate 1 is connected with L-shaped fixed plate 2, the bottom of the L-shaped fixed plate 2 is rotatably connected with simulated missile clamping part 3, the outer side of the top of the L-shaped fixed plate 2 is detachably connected with rotating connecting piece 4, one end of the top of the rotating connecting piece 4 is detachably connected with telescopic connecting shaft 5, the other end of the telescopic connecting shaft 5 is detachably connected with combination clamp 6, the outer side of the first fixed plate 1 is symmetrically connected with the rotating connecting piece 4, the telescopic connecting shaft 5 and the combination clamp 6, the combination clamp 6 is detachably connected with the unmanned helicopter support, when the device is installed, select the appropriate unmanned helicopter support as the supporting installation point, the unmanned helicopter support can select the landing gear with high structural strength, the original carrier platform, the body frame and other parts convenient to install, after selecting the relatively triangularly distributed installation support points on the unmanned helicopter support, measure the distance size of the three installation support points to the corresponding installation holes of the pod, then adjust the telescopic connecting shaft 5 to the corresponding length, the size error can be controlled within 3cm, connect the connecting end of the combination clamp 6 with the telescopic connecting shaft 5, finally connect the clamping end of the combination clamp 6 with the unmanned helicopter support, and adjust the L-shaped fixed plate 2 to be horizontal with the horizontal plane of the unmanned helicopter, since the three telescopic connecting shafts 5 are arranged in a triangular shape, the stability of the L-shaped fixed plate can be improved, and the stability of the simulated missile clamping part 3 can be ensured, which is convenient for subsequent simulated missile experiments, and the length of the telescopic connecting shaft 5 can be adjusted according to the condition of the unmanned helicopter support, thereby being suitable for unmanned helicopters of different specifications, the manufacturing cost is low, the installation and disassembly are convenient, and the simulated bomb dropping training of unmanned helicopters of different specifications is suitable.
[0036] Please refer to Figure 3 The rotating connecting piece 4 includes a fixed pin 41, one end of the fixed pin 41 is threadedly connected with a first bolt 42, the other end of the fixed pin 41 is connected with a concave clamping piece 43, the concave clamping piece 43 is detachably connected with the telescopic connecting shaft 5, the rotating connecting piece 4 can be detachably connected with the L-shaped fixed plate 2 and the first fixed plate 1, and can rotate at any angle, when installed, align the fixed pin 41 with the preset hole position on the L-shaped fixed plate 2 and the first fixed plate 1, and then insert the first bolt 42 into the hole position and rotate the fixed pin 41 to connect.
[0037] Please refer to Figure 3Threaded connection first connecting piece 51 one end of the telescopic connecting shaft 5 both ends, the first connecting piece 51 the other end of the rotating block 52 is integrally formed, the rotating block 52 through the bolt and the female joint 43 can be detachable connection, telescopic connecting shaft 5 both ends are threaded end, threaded end can be rotated into the first connecting piece 51 one end and rotating installation, then in the female joint 43 through the bolt connection, in the female joint 43 can be rotated within a certain angle range, cooperate with the L-shaped fixed plate 2 and the first fixed plate 1 installation positioning.
[0038] Please focus on Figure 2 , the telescopic connecting shaft 5 includes the first telescopic pipe 53, the first telescopic pipe 53 one end sliding plug second telescopic pipe 54, the first telescopic pipe 53 and second telescopic pipe 54 on the interval has fixed hole 55, the fixed hole 55 through the screw connection, first telescopic pipe 53 and second telescopic pipe 54 between each other cooperation sliding, can be within a certain range of telescopic, telescopic in the appropriate fixed hole 55 installation screw fixed, further adapt to different specifications and size of unmanned helicopter support.
[0039] Please focus on Figure 4 , the combination of hoop 6 includes symmetrically arranged arc joint 61, the arc joint 61 both sides are provided with clamping hole 62, one of the clamping hole 62 and the rotating block 52 through the bolt connection, need to install the device, can be connected with the unmanned helicopter support, one clamping hole 62 through the bolt fixed, the other clamping hole 62 and rotating block 52 alignment after through the bolt fixed, can complete the connection with the unmanned helicopter support.
[0040] The arc joint 61 and the unmanned helicopter support connection is equipped with buffer material, buffer material uses rubber gasket, foam gasket and other materials, improve the locking degree and connection stability.
[0041] Please focus on Figure 1The simulation missile clamping part 3 comprises a mounting block 31, the mounting block 31 is connected with the L-shaped fixing plate 2 and the first fixing plate 1 through a rotating column 32 at both ends, the mounting block 31 is provided with assembly holes 33 at intervals, one side of the assembly holes 33 is connected with a shell mounting pipe 34, simulation rocket shells are placed in the shell mounting pipe 34, the simulation missile clamping part 3 is used for mounting simulation rocket shells, when mounting, the simulation rocket shells are inserted into the shell mounting pipe 34, the rotating column 32 and the mounting block 31 can be connected in a damping mode, so that the angle of the mounting block 31 is adjusted, and a firing output cable is arranged at the rear end of each simulation rocket shell, the firing output cables are wound together and connected with a firing control receiving module, the firing control receiving module is mounted at a suitable position of the unmanned helicopter, and the launching time of the simulation rocket shells can be controlled through a wireless mode when the unmanned helicopter takes off, and it should be noted that the firing control receiving module, the wireless launching device and the simulation rocket shells adopt the prior art, and details are not described herein.
[0042] Please refer to Figure 1 The shell mounting pipe 34 is provided with a fixing notch, the fixing notch is screw-connected with a limiting bolt 341, and after the simulation rocket shell is mounted in the limiting bolt 341, the simulation rocket shell is further fixed through the limiting bolt 341, so that the simulation rocket shell is prevented from falling accidentally.
[0043] Please refer to Figure 1 The L-shaped fixing plate 2 is provided with an arc-shaped groove 21 on the side, the arc-shaped groove 21 is matched and connected with a locking screw 22, and the locking screw 22 is connected with the mounting block 31 at the end, since different training targets need to be attacked at different heights, the missile discharging angle of the simulation rocket shells needs to be set to different angles, after the angle of the mounting block 31 is adjusted through the arc-shaped groove 21 matched with the locking screw 22, the angle is fixed through the locking screw 22, and a rubber pad is arranged at the intersection of the locking screw 22 and the mounting block 31, so that the friction is increased.
[0044] The above-described embodiments only express certain implementation manners of the present application, and the description is relatively specific and detailed, but the present application should not be understood as being limited in the patent scope; it should be pointed out that, for ordinary skilled persons in the art, some modifications and improvements can be made without departing from the concept of the present application, and these all belong to the protection scope of the present application; therefore, the protection scope of the present application should be subject to the appended claims.
Claims
1. An easy-to-install unmanned helicopter airborne pod, characterized in that: The first fixing plate (1) is connected to an L-shaped fixing plate (2) on one side of its top. The bottom of the L-shaped fixing plate (2) is rotatably connected to a simulated missile clamping part (3). The top outer side of the L-shaped fixing plate (2) is detachably connected to a rotating connector (4). The top of the rotating connector (4) is detachably connected to one end of a telescopic connecting shaft (5). The other end of the telescopic connecting shaft (5) is detachably connected to a coupling clamp (6). The rotating connector (4), the telescopic connecting shaft (5), and the coupling clamp (6) are symmetrically connected to the outside of the first fixing plate (1). The coupling clamp (6) is detachably connected to the unmanned helicopter support.
2. The easily installable unmanned helicopter airborne pod according to claim 1, characterized in that: The rotating connector (4) includes a fixing pin (41), one end of which is threaded to a first bolt (42), and the other end of which is connected to a concave snap-fit (43). The concave snap-fit (43) is detachably connected to the telescopic connecting shaft (5).
3. The easily installable unmanned helicopter airborne pod according to claim 2, characterized in that: The telescopic connecting shaft (5) is threaded to one end of the first connecting piece (51) at both ends. The other end of the first connecting piece (51) is integrally formed with the rotating block (52). The rotating block (52) is detachably connected to the concave snap-fit piece (43) by bolts.
4. The easily installable unmanned helicopter airborne pod according to claim 3, characterized in that: The telescopic connecting shaft (5) includes a first telescopic tube (53), one end of which is slidably inserted into a second telescopic tube (54). The first telescopic tube (53) and the second telescopic tube (54) are spaced apart by fixing holes (55), which are connected by screws.
5. The easily installable unmanned helicopter airborne pod according to claim 4, characterized in that: The combined clamp (6) includes symmetrically arranged arc-shaped snap-fit parts (61), and snap-fit holes (62) are provided on both sides of the arc-shaped snap-fit parts (61). One of the snap-fit holes (62) is connected to the rotating block (52) by bolts.
6. The easily installable unmanned helicopter airborne pod according to claim 5, characterized in that: The arc-shaped snap-fit connector (61) is provided with cushioning material at the connection point with the unmanned helicopter support.
7. The easily installable unmanned helicopter airborne pod according to claim 1, characterized in that: The simulated missile clamping part (3) includes a mounting block (31). The two ends of the mounting block (31) are connected to the L-shaped fixing plate (2) and the first fixing plate (1) through rotating columns (32). The mounting block (31) has assembly holes (33) spaced apart. One side of the assembly hole (33) is connected to the ammunition installation tube (34). The ammunition installation tube (34) contains a simulated rocket.
8. The easily installable unmanned helicopter airborne pod according to claim 7, characterized in that: The ammunition mounting tube (34) has a fixing notch, and the fixing notch is threadedly connected to a limiting bolt (341).
9. The easily installable unmanned helicopter airborne pod according to claim 7, characterized in that: The L-shaped fixing plate (2) has an arc groove (21) on its side, and the arc groove (21) is matched and connected to a locking screw (22). The end of the locking screw (22) is connected to the mounting block (31).